Nodal Period of an Earth Satellite

Description:Calculates the nodal period of a satellite using a numerical integration technique. The algorithm first uses the RKF78 method to propagate the first-order perturbed equations of satellite motion forward in time to bracket a "nodal objective function". Once a bracket is found, the algorithm then uses Brent's root-finding method to find the time at which the objective function is zero to within a user-defined tolerance. While looking for the root the software also uses the RKF78 method to propagate the satellite's orbit subject to the main oblateness gravity perturbation of the Earth.
Filename:tnodal.zip
ID:9491
Author:C. Deagle, Jr.
Downloaded file size:242,752 bytes
Size on calculator:43 KB
Platforms:Prime  
User rating:Not yet rated (you must be logged in to vote)
Primary category:Science
Languages:ENG  
File date:2022-10-20 17:32:08
Creation date:2022-10-20
Source code:Included
Download count:88
Version history:2023-05-29: Added to site
Archive contents:
  Length      Date    Time    Name
---------  ---------- -----   ----
   247318  2012-12-20 08:09   periods.pdf
    43958  2022-10-20 15:51   tnodal.hpprgm
     4458  2022-10-20 17:32   tnodal.html
    20742  2022-10-20 15:52   tnodal.txt
---------                     -------
   316476                     4 files
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